{"meta":{"query_hash":"1ace1c82d930","filters":{"venue":"International Journal of Turbo and Jet Engines"},"cohort_total":6,"direct_labels_cover":0,"predictions_cover":6,"exported":6,"export_cap":100000,"truncated":false,"label_status":"direct model label, unvalidated","prediction_status":"machine_predicted_unvalidated (Codex and Gemma teacher distillation)","score_status":"score_only:v0-immature-baseline","snapshot":{"source":"OpenAlex, pinned release, all 482 partitions","release":"2026-06-24","frame_built":"2026-07-12"},"permalink":"https://metacan.xera.ac/q/1ace1c82d930","api":"https://metacan.xera.ac/api/v1/cohort?venue=International+Journal+of+Turbo+and+Jet+Engines"},"results":[{"id":"W2565811154","doi":"10.1515/tjj-2015-0052","title":"Numerical Study of the Propulsive Performance of the Hollow Rotating Detonation Engine with a Laval Nozzle","year":2015,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Combustion and Detonation Processes","field":"Engineering","cited_by":16,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Nozzle; Detonation; Thrust; Rocket engine nozzle; Specific impulse; Mechanics; Propulsive efficiency; Impulse (physics); Mass flow rate; Aerospace engineering; Materials science; Mechanical engineering; Physics; Engineering; Chemistry; Classical mechanics; Explosive material","score_opus":0.009974556220167838,"score_gpt":0.2238339786969961,"score_spread":0.21385942247682826,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2565811154","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9982832,0.00015593323,0.000626674,0.00024447328,0.0004902417,0.00008801599,0.0000024397057,0.000008527867,0.00010047597],"genre_scores_gemma":[0.9995322,0.000018189708,0.00030598463,0.0000146517805,0.00008501416,0.0000027655426,4.0451064e-7,0.0000074013046,0.00003334975],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.99915725,0.000019412042,0.00027114653,0.0000439498,0.0004588679,0.00004937391],"domain_scores_gemma":[0.99901104,0.000047328424,0.00018500944,0.00005894673,0.0006695011,0.00002818308],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00014388439,0.00007416935,0.00011706346,0.00008089645,0.00002002536,0.000016030786,0.00021177906,0.000018377166,0.0000043051473],"category_scores_gemma":[0.0001423289,0.0000381957,0.0000345179,0.00015807914,0.000025232473,0.00016414918,0.000026588828,0.00011769601,1.6702944e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00022896338,0.000285474,0.29998073,0.000095524374,0.0003236488,0.000005107457,0.0056372085,0.6705415,0.0012872255,0.00011489096,0.00024913403,0.021250583],"study_design_scores_gemma":[0.0061469297,0.0012012318,0.49145654,0.0007431861,0.00015475665,0.0005278281,0.003106739,0.41957384,0.07515029,0.00024772633,0.0013407063,0.00035021716],"about_ca_topic_score_codex":0.000007744655,"about_ca_topic_score_gemma":0.0000077729765,"teacher_disagreement_score":0.25096765,"about_ca_system_score_codex":0.000020565805,"about_ca_system_score_gemma":0.000047992657,"threshold_uncertainty_score":0.15575753},"labels":[],"label_agreement":null},{"id":"W2621079678","doi":"10.1515/tjj-2017-0010","title":"Optimization Design and Experimental Study of a Two-disk Rotor System Based on Multi-Island Genetic Algorithm","year":2017,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Magnetic Bearings and Levitation Dynamics","field":"Engineering","cited_by":10,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"Queen's University","funders":"","keywords":"Critical speed; Rotor (electric); Helicopter rotor; Amplitude; Vibration; Genetic algorithm; Position (finance); Control theory (sociology); Computer science; Optimal design; Range (aeronautics); Engineering; Algorithm; Acoustics; Physics; Mechanical engineering; Aerospace engineering; Optics; Artificial intelligence","score_opus":0.013449504157558936,"score_gpt":0.2589834333930931,"score_spread":0.24553392923553416,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2621079678","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.59046024,0.00023544156,0.40850666,0.000023401177,0.00053000386,0.00016808479,0.000008203869,0.000011957024,0.000055990575],"genre_scores_gemma":[0.9280417,0.00002267367,0.071804576,0.0000046678533,0.000100223544,0.000005120485,9.271246e-7,0.0000102944,0.000009801598],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99944466,0.00001913169,0.00023339683,0.00006481144,0.00018582563,0.000052184856],"domain_scores_gemma":[0.999574,0.00004587614,0.00014523292,0.00007180839,0.00012127265,0.000041814288],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00011303532,0.000089195826,0.00013376235,0.00011759469,0.00003814436,0.00009227375,0.00012952057,0.00002394515,0.000011345097],"category_scores_gemma":[0.000024075049,0.00007358046,0.000023958339,0.000012923974,0.000018728497,0.00009687225,0.000016383072,0.000060603794,1.5563677e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000034239205,0.000115326504,0.0020689252,0.000019342044,0.00006819971,0.000021917378,0.00035437397,0.992611,0.00027659716,0.000011879544,0.000011466374,0.0044067204],"study_design_scores_gemma":[0.0022549974,0.00032735209,0.007807517,0.000090117974,0.00001992778,0.000034505025,0.00020928842,0.9887072,0.0004677118,0.000003004364,0.000009372281,0.00006903882],"about_ca_topic_score_codex":0.000016425862,"about_ca_topic_score_gemma":0.0000023607797,"teacher_disagreement_score":0.33758146,"about_ca_system_score_codex":0.000021344604,"about_ca_system_score_gemma":0.0000074610775,"threshold_uncertainty_score":0.3000524},"labels":[],"label_agreement":null},{"id":"W2969191831","doi":"10.1515/tjj-2019-0024","title":"Numerical Investigation on the Effects of Vortex Generator Locations on Film Cooling Performance","year":2019,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Turbomachinery Performance and Optimization","field":"Engineering","cited_by":8,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"University of Toronto","funders":"","keywords":"Vortex; Upstream (networking); Materials science; Vortex generator; Optics; Flow (mathematics); Mechanics; Physics; Telecommunications; Engineering","score_opus":0.005346417291468347,"score_gpt":0.1936539644904711,"score_spread":0.18830754719900275,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2969191831","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99722993,0.00020279015,0.00083068217,0.0002371366,0.001229184,0.00006433992,0.0000023453326,0.00001352843,0.0001900734],"genre_scores_gemma":[0.9988597,0.00037718305,0.00023238266,0.00019399416,0.00028529234,0.0000025601043,0.000005151147,0.0000103849325,0.00003333438],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9994415,0.000012426894,0.00021731814,0.0000507852,0.00021480561,0.000063171705],"domain_scores_gemma":[0.99949443,0.00019218285,0.00009177377,0.00006555978,0.00012585687,0.000030163861],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00009208657,0.00008759857,0.000107020714,0.00012670853,0.00002185976,0.000023803044,0.00013017342,0.000033147066,0.000018790215],"category_scores_gemma":[0.00007204756,0.000056422257,0.000038130205,0.00007320899,0.000015787013,0.00017918907,0.0000070943097,0.00014234352,0.000007827765],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.000045630688,0.000022081585,0.01591067,0.00007105575,0.00009593006,0.0000019386803,0.00026176192,0.9741268,0.0047492324,0.0006464772,0.00071798894,0.0033504355],"study_design_scores_gemma":[0.00054797676,0.00027657312,0.05224041,0.0004170408,0.000020192776,0.000029272318,0.000022708986,0.86967236,0.0756837,0.0000701666,0.00089392,0.0001257128],"about_ca_topic_score_codex":0.000001435839,"about_ca_topic_score_gemma":2.6823724e-7,"teacher_disagreement_score":0.104454465,"about_ca_system_score_codex":0.000024091374,"about_ca_system_score_gemma":0.000014233159,"threshold_uncertainty_score":0.23008329},"labels":[],"label_agreement":null},{"id":"W2996297201","doi":"10.1515/tjj-2016-0067","title":"A Preliminary Design System for Turbine Discs","year":2017,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Manufacturing Process and Optimization","field":"Engineering","cited_by":3,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure","funders":"Natural Sciences and Engineering Research Council of Canada","keywords":"Finite element method; Turbine; CAD; Parameterized complexity; Computer science; Rotor (electric); Software; Reduction (mathematics); Computer Aided Design; Mechanical engineering; Design tool; Engineering; Engineering drawing; Automotive engineering; Structural engineering","score_opus":0.016049623864332355,"score_gpt":0.24320367312317556,"score_spread":0.2271540492588432,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W2996297201","genre_codex":"methods","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":null,"domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.10046389,0.00210622,0.8909565,0.00097061,0.004678485,0.00019425584,0.000026607277,0.00008203665,0.0005213458],"genre_scores_gemma":[0.9900248,0.00019754842,0.009102348,0.0000071514796,0.00057806383,0.000004971352,0.0000024819926,0.000012750265,0.000069850365],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.9995841,0.000003853883,0.00017968321,0.000048626425,0.00011631022,0.00006746638],"domain_scores_gemma":[0.9995747,0.000047499896,0.00011751101,0.00006604349,0.00015636339,0.00003783192],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00012013809,0.00007944598,0.000112907146,0.00007480962,0.000056048062,0.00014534613,0.00023261656,0.000033658573,0.0000040533914],"category_scores_gemma":[0.000064518244,0.000059804617,0.00004506658,0.0000065983095,0.000013032647,0.00027043122,0.000019396906,0.000055383163,4.5412293e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.0005268301,0.000048021924,0.0013428355,0.00063238374,0.00053798995,0.00008420411,0.00068706006,0.92363334,0.0009133035,0.0014531085,0.0030330499,0.06710788],"study_design_scores_gemma":[0.003272993,0.00042376382,0.016629072,0.0012258289,0.00015085255,0.0007048349,0.00017055735,0.9117305,0.051281665,0.0012960141,0.012638502,0.00047539885],"about_ca_topic_score_codex":0.000002037892,"about_ca_topic_score_gemma":3.4881862e-7,"teacher_disagreement_score":0.88956094,"about_ca_system_score_codex":0.000023802422,"about_ca_system_score_gemma":0.000008011119,"threshold_uncertainty_score":0.24387616},"labels":[],"label_agreement":null},{"id":"W4366139317","doi":"10.1515/tjj-2022-0073","title":"Effect of zero penetration angle chevrons in supersonic jet noise and screech tone mitigation","year":2023,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Aerodynamics and Acoustics in Jet Flows","field":"Engineering","cited_by":5,"is_retracted":false,"has_abstract":true,"route_ca_aff":false,"route_ca_fund":false,"route_ca_venue":false,"route_about_ca":true,"ca_institutions":"","funders":"","keywords":"Mach number; Supersonic speed; Physics; Nozzle; Acoustics; Schlieren; Noise (video); Penetration (warfare); Optics; Schlieren imaging; Mechanics; Engineering","score_opus":0.004473665508924468,"score_gpt":0.24611320484382204,"score_spread":0.24163953933489757,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4366139317","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.99743366,0.00049422926,0.0012367286,0.0001337381,0.0004989456,0.000050274484,0.000019182306,0.00001678201,0.000116436466],"genre_scores_gemma":[0.9985318,0.0009243789,0.0003476759,0.000006505183,0.00014271843,0.0000019862641,0.00001538605,0.000011319251,0.000018226696],"study_design_codex":"simulation_or_modeling","study_design_gemma":"simulation_or_modeling","domain_scores_codex":[0.99941933,0.000016467786,0.00024374263,0.000060545142,0.0001771632,0.0000827508],"domain_scores_gemma":[0.9996421,0.00014783617,0.000052492305,0.000038828748,0.00008351579,0.000035239504],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00031487865,0.000089920555,0.00015240487,0.00020226096,0.000011885799,0.000027607242,0.000086848864,0.000049844646,0.0000070331166],"category_scores_gemma":[0.00009685409,0.000075097254,0.00003719361,0.00010880051,0.000023747218,0.00015353401,0.000019316794,0.000118123455,8.332661e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":"simulation_or_modeling","about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00029926142,0.000105787534,0.18541591,0.0006592588,0.0006058227,0.00025569985,0.0019870766,0.367604,0.36299607,0.0019165629,0.0020554864,0.07609907],"study_design_scores_gemma":[0.0024526312,0.0004596693,0.16195668,0.0005187634,0.00007149184,0.00017098367,0.00014766505,0.80031693,0.032035165,0.0012993546,0.0002791003,0.0002915548],"about_ca_topic_score_codex":0.000009653217,"about_ca_topic_score_gemma":0.000020092933,"teacher_disagreement_score":0.43271294,"about_ca_system_score_codex":0.00002911854,"about_ca_system_score_gemma":0.000009030262,"threshold_uncertainty_score":0.30623773},"labels":[],"label_agreement":null},{"id":"W4383555327","doi":"10.1515/tjj-2021-0048","title":"Numerical study of the impact of hydrogen addition, swirl intensity and equivalence ratio on methane-air combustion","year":2023,"lang":"en","type":"article","venue":"International Journal of Turbo and Jet Engines","topic":"Combustion and flame dynamics","field":"Engineering","cited_by":1,"is_retracted":false,"has_abstract":true,"route_ca_aff":true,"route_ca_fund":true,"route_ca_venue":false,"route_about_ca":false,"ca_institutions":"École de Technologie Supérieure; Université du Québec à Montréal","funders":"Compute Canada","keywords":"Combustor; Combustion; Hydrogen; Intensity (physics); Materials science; Turbulence; Methane; Gas turbines; Range (aeronautics); Environmental science; Nuclear engineering; Mechanics; Chemistry; Mechanical engineering; Engineering; Composite material; Organic chemistry; Physics; Optics","score_opus":0.01471371527141146,"score_gpt":0.27139168429555915,"score_spread":0.2566779690241477,"validation_status":"score_only:v0-immature-baseline","prediction":{"id":"W4383555327","genre_codex":"empirical","genre_gemma":"empirical","domain_codex":null,"domain_gemma":null,"model_version":"codex-gemma-dda1882f352a","genre_candidate":"empirical","genre_consensus":"empirical","domain_candidate":null,"domain_consensus":null,"prediction_status":"machine_predicted_unvalidated","genre_scores_codex":[0.9987338,0.000056725316,0.00055644213,0.00012173134,0.00040355447,0.00005984694,0.000024051897,0.000015722204,0.000028084742],"genre_scores_gemma":[0.9997471,0.00011771866,0.000023383165,0.000009157387,0.00007758897,9.4321166e-7,0.0000045304723,0.0000068197683,0.000012757545],"study_design_codex":"simulation_or_modeling","study_design_gemma":"observational","domain_scores_codex":[0.9993578,0.000025581825,0.00027267137,0.000053124935,0.00023314678,0.000057666704],"domain_scores_gemma":[0.9994144,0.00010513825,0.00011789592,0.00006500888,0.00026322075,0.00003433688],"candidate_categories":[],"consensus_categories":[],"category_scores_codex":[0.00015983875,0.000082777224,0.0001671702,0.00016906702,0.000015460166,0.000008912809,0.0001290431,0.000028409811,0.000013331033],"category_scores_gemma":[0.000118315715,0.000054558648,0.00007677795,0.0001437529,0.000032158838,0.00009015581,0.000032272153,0.00012822097,6.1227183e-7],"study_design_candidate":"simulation_or_modeling","study_design_consensus":null,"about_ca_topic_candidate":false,"about_ca_topic_consensus":false,"about_ca_system_candidate":false,"about_ca_system_consensus":false,"study_design_scores_codex":[0.00020379739,0.0002169647,0.051401567,0.000037177837,0.0006242167,0.000020647674,0.0012998139,0.93223,0.0073331133,0.00020841636,0.0010269707,0.005397336],"study_design_scores_gemma":[0.0012573178,0.0005429426,0.6250633,0.00020222836,0.000057926696,0.00014981964,0.0004453875,0.36652002,0.005079784,0.0005135943,0.000037068887,0.00013061764],"about_ca_topic_score_codex":0.00001763917,"about_ca_topic_score_gemma":0.000002921625,"teacher_disagreement_score":0.57366174,"about_ca_system_score_codex":0.0000316883,"about_ca_system_score_gemma":0.000013203781,"threshold_uncertainty_score":0.22248371},"labels":[],"label_agreement":null}]}